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现代战斗机的英文

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"现代战斗机"怎么读用"现代战斗机"造句

英文翻译手机手机版

  • present-day fighter

例句与用法

  • Development of firepower control system on modern fighter
    机载火力控制系统在现代战斗机上的发展
  • Modern fighter planes fly at incredible speeds , and can cross entire continents and oceans in very little time
    现代战斗机飞行速度相当惊人,能在很短的时间内飞越整个大陆与海洋。
  • For the need of fight , the fight aircraft have flexibility , promptness and the ability of hiding , but the three are incompatible
    现代战斗机为适应空战的需要必须具有高度的敏捷性,机动性和隐身性,但这三者之间存在着不可调和的矛盾。
  • Modern low bypass ratio turbofan engine is the heart of the new fighter , whose performance and aerodynamic stability greatly affect the characteristics of the new fighter
    涡扇发动机作为现代战斗机的心脏,其性能和稳定性对战斗机的性能和稳定性能有很大的影响。
  • The study proves that the structure of the modern fighter simulation system is reasonable , and has built the solid base for the further study
    研究结论表明现代战斗机仿真系统结构与接口是合理的,并且能够满足现代战斗机设计与验证的要求,并为今后进一步研究打下了坚实的基础。
  • Therefore , in this paper the multi - objective optimization design of aerodynamic and stealthy configuration for the fighter is discussed according to the geometrical characteristics of the advanced tactical fighter . the work is performed as follows : 1 according to the different design requirement in subsonic and supersonic state , with the multi - objective optimization method , the aerodynamic configuration optimization method for different design requirements has been obtained
    基于以上考虑,本文从研究气动隐身多目标优化问题的角度出发,针对先进战斗机的外形设计特点,完成了以下工作: 1 、针对现代战斗机亚、超音速的不同设计要求,利用多目标优化设计方法建立了可进行满足不同设计要求的气动外形优化设计方法。
  • This thesis first states the characteristics of the equipments that have been adopted by the modern fighter and their basic technical performance . then an overall layered modular design for air combat simulation system is made utilizing system simulation technology and critical sub - systems have been mathematically modeled known as fighter body , propulsive system , flight control system , radar , fire control system , gun , air - air missile and avionics . after that a set of distributed air combat simulation system software is developed based on the scene graphics pc platform
    本文首先介绍了现代战斗机空战技术装备及其基本技术性能特点;而后使用系统仿真技术,依据分层模块化设计思想,制定了空战仿真系统总体设计方案;之后根据目前技术状况,建立了战斗机机体、推进系统、飞控系统、雷达、火控系统、航炮、空空导弹、航电设备等战斗机关键子系统数学模型;在此基础上,根据总体设计方案,在基于pc的分布交互式视景仿真平台上开发了一套分布式空战仿真系统软件,实现了战斗机交互式飞行仿真和分布式空战仿真。
  • The thesis describes the conception of the object - oriented modeling and integrated simulaton enviroment , and discusses the below topics : ( 1 ) describe the reasonable structure of the modern fighter simulation system , and design the data transfer interface . ( 2 ) discuss the modeling method of the key subsystem of future fighter system especially the aerodynamics and the control system in detail . ( 3 ) construct the 3d model of the aircraft and scene , and verify the graphic simulation technique based on pc
    本文详细讨论了面向对象建模方法以及一体化仿真环境的基本概念框架及基本结构并在此基础上提出了合理的现代战斗机仿真系统结构,设计了仿真系统的数据传递接口;详细讨论了现代战斗机仿真系统关键子系统? ?飞机本体、飞行控制系统建模方法;建立了用于研究的飞机以及视景的三维显示平台;并在此基础上实现了实验性的基于pc的现代战斗机图形仿真平台,对仿真模型有效性确认和验证工作做了初步的探讨,研究比较了传统飞行动力学和运动学方程和四元数法在飞行仿真中的效果。
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